The invention provides a dual-interface
satellite-borne
signal transmitting and receiving
system, which at least comprises two groups of mutually independent
signal transmitting and receiving channels in redundant configuration, any
signal transmitting and receiving channel comprises a transmitting and receiving interface
chip assembly, an
external interface, a
peripheral configurable circuit and a controller, the transmitting and receiving interface
chip assembly is used for transmitting and / or receiving differential signals, and the
external interface is used for receiving and transmitting the differential signals. The
external interface is used for being electrically connected with a differential connector outside the spaceborne equipment, and the
peripheral configurable circuit is electrically connected with the transceiving interface
chip assembly and the external interface and is used for performing
coupling,
impedance matching, amplitude limiting protection and / or fault isolation on the signal transceiving channel based on different configuration conditions. And the controller is electrically connected with the transceiving interface chip assembly through a
peripheral configurable circuit and is used for enabling acquisition
processing or sending
processing of differential data. According to the invention, dual-interface compatibility, dual-channel redundancy and configurable and reconfigurable peripheral networks are realized on the same hardware platform, and the
satellite-borne signal receiving and transmitting
system is adaptive to various external wiring
modes.